SHOCK WAVE INTERACTION STUDIES IN A DOUBLE-ENDED OPPOSING DRIVER ELECTROMAGNETIC SHOCK TUBE,

Abstract

The head-on collisions of Mach 20 - 23 ionizing shock waves in argon at an initial pressure of 115 microns Hg were experimentally investigated. The shock wave collisions were created in a double-ended opposing driver electromagnetic shock tube. Shock wave speeds were obtained using photometric techniques. Plasma time-resolved atom and ion number densities and temperatures were obtained from spectroscopic analysis of emission radiation using a spectrograph equipped with a photoelectric attachment. Photographs of visible luminous phenomena associated with the incident shock waves and shock wave collisions were obtained with an image converter camera. The plasma behind the incident shock waves was found to be a mixture of driver and driven gas. Correlation of photographic and spectroscopic results for shock wave collisions indicated that reflected shock wave/incident shock wave boundary layer interaction occurred resulting in reflected shock wave bifurcation. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1968
Accession Number
AD0680834

Entities

People

  • David A. Freiwald

Organizations

  • Northwestern University

Tags

DTIC Thesaurus Topics

  • Boundary Layer
  • Cameras
  • Collisions
  • Converters
  • Image Converters
  • Images
  • Photographs
  • Photography
  • Shock
  • Shock Tubes
  • Shock Waves
  • Tubes
  • Waves

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Plasma Physics.